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Home > Reference > Research and information: general > Research methods: general > Comparison of Pressure Distributions on Model and Full-Scale NACA 64-621 Airfoils with Ailerons for Wind Turbine Application
Comparison of Pressure Distributions on Model and Full-Scale NACA 64-621 Airfoils with Ailerons for Wind Turbine Application

Comparison of Pressure Distributions on Model and Full-Scale NACA 64-621 Airfoils with Ailerons for Wind Turbine Application


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About the Book

The aerodynamic similarity between a small (4-inch chord) wind tunnel model and a full-scale wind turbine blade (24-foot tip section with a 36-inch chord) was evaluated by comparing selected pressure distributions around the geometrically similar cross sections. The airfoils were NACA 64-621 sections, including trailing-edge ailerons with a width equal to 38 percent of the airfoil chord. The model airfoil was tested in the OSU 6- by 12-inch High Reynolds Number Wind Tunnel; the full-scale blade section was tested in the NASA Langley Research Center 30- by 60-foot Subsonic Wind Tunnel. The model airfoil contained 61 pressure taps connected by embedded tubes to pressure transducers. A belt containing 29 pressure taps was fixed to the full-scale section at midspan to obtain surface pressure data. Lift coefficients were obtained by integrating pressures, and corrections were made for the 3-D effects of blade twist and downwash in the blade tip section. The results of the two different experimental methods correlated well for angles of attack from minus 4 to 36 degrees and aileron reflections from 0 to 90 degrees. Gregorek, G. M. and Kuniega, R. J. and Nyland, T. W. Glenn Research Center NASA-TM-100802, DOE/NASA/20320-75, E-3982, NAS 1.15:100802 DE-AI01-76ET-20320; RTOP 776-33-41...


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Product Details
  • ISBN-13: 9781725577435
  • Publisher: Createspace Independent Publishing Platform
  • Publisher Imprint: Createspace Independent Publishing Platform
  • Height: 279 mm
  • No of Pages: 30
  • Spine Width: 2 mm
  • Width: 216 mm
  • ISBN-10: 1725577437
  • Publisher Date: 16 Aug 2018
  • Binding: Paperback
  • Language: English
  • Returnable: N
  • Weight: 95 gr


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Comparison of Pressure Distributions on Model and Full-Scale NACA 64-621 Airfoils with Ailerons for Wind Turbine Application
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